Pietenpol-List: Re: Don Mosher's Long Fuse posting
Posted: Fri Jun 16, 2000 8:10 am
Original Posted By: "Greg Yotz"
Don, That was a very good posting about the wing placement on the Piet. It has always bothered me about angling the cabane struts to move the wing around a lot. I like the idea of lift forces being transferred from the wing thru straight cabanes struts into the fuselage, it seems to me that there are less side forces on the cabanes and you'll get full advantage of their strength. Saying that, I fully expect to use the ability to move the wing to fine tune my wing placement. Heck, I'm still an amateur builder, and I expect to make some errors, but I hope that the struts will be more or less vertical. I also don't think I've heard of any Piets going down due to structural failure in this area, so I don't know that it's a big safety issue, angle or not. I also have the feeling that this is one of those quirky Piet things where it's okay NOT to conform to traditional design standards! I've kinda wondered for awhile that the statement about the Piet not coming out of a slip is more a problem with the one-piece wing being straight with no positive dihedral combined with the smallish vertical tail-surface area. I plan to build the 3 piece wing with a little positive dihedral to insure stability and it looks a little better. I had thought about slightly enlarging the vertical tail surfaces, but I figure there are a lot of Piets out there with the smaller one, plus, it would add more weight to the tail which for me is a no-no, So I built the traditional size vertical stab/rudder. Don, I'm sure your posting will generate a good bit of spirited discussion on the list here, and that's a good thing, stuff like this gets the rest of us off our duff, and excited again, (along with Stevee's morning-flight posting - nice one Steve, wish I could have been there. Gordon Baxter would have been proud...). I think I'll go out this weekend and work on my horizontal stab/elevators some!Thanks!Gary Meadows________________________________________________________________________________
Don, That was a very good posting about the wing placement on the Piet. It has always bothered me about angling the cabane struts to move the wing around a lot. I like the idea of lift forces being transferred from the wing thru straight cabanes struts into the fuselage, it seems to me that there are less side forces on the cabanes and you'll get full advantage of their strength. Saying that, I fully expect to use the ability to move the wing to fine tune my wing placement. Heck, I'm still an amateur builder, and I expect to make some errors, but I hope that the struts will be more or less vertical. I also don't think I've heard of any Piets going down due to structural failure in this area, so I don't know that it's a big safety issue, angle or not. I also have the feeling that this is one of those quirky Piet things where it's okay NOT to conform to traditional design standards! I've kinda wondered for awhile that the statement about the Piet not coming out of a slip is more a problem with the one-piece wing being straight with no positive dihedral combined with the smallish vertical tail-surface area. I plan to build the 3 piece wing with a little positive dihedral to insure stability and it looks a little better. I had thought about slightly enlarging the vertical tail surfaces, but I figure there are a lot of Piets out there with the smaller one, plus, it would add more weight to the tail which for me is a no-no, So I built the traditional size vertical stab/rudder. Don, I'm sure your posting will generate a good bit of spirited discussion on the list here, and that's a good thing, stuff like this gets the rest of us off our duff, and excited again, (along with Stevee's morning-flight posting - nice one Steve, wish I could have been there. Gordon Baxter would have been proud...). I think I'll go out this weekend and work on my horizontal stab/elevators some!Thanks!Gary Meadows________________________________________________________________________________